CN115079297A - Water source detection device for underground water source detection - Google Patents

Water source detection device for underground water source detection Download PDF

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Publication number
CN115079297A
CN115079297A CN202210756781.1A CN202210756781A CN115079297A CN 115079297 A CN115079297 A CN 115079297A CN 202210756781 A CN202210756781 A CN 202210756781A CN 115079297 A CN115079297 A CN 115079297A
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CN
China
Prior art keywords
water source
flight
fixedly connected
remote controller
gear
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Pending
Application number
CN202210756781.1A
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Chinese (zh)
Inventor
孙丽
张亚
王国庆
杜俊洋
李勖之
陆晓松
冯艳红
郑丽萍
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Nanjing Institute of Environmental Sciences MEE
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Nanjing Institute of Environmental Sciences MEE
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Priority to CN202210756781.1A priority Critical patent/CN115079297A/en
Publication of CN115079297A publication Critical patent/CN115079297A/en
Pending legal-status Critical Current

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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V9/00—Prospecting or detecting by methods not provided for in groups G01V1/00 - G01V8/00
    • G01V9/02—Determining existence or flow of underground water
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S15/00—Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
    • G01S15/86—Combinations of sonar systems with lidar systems; Combinations of sonar systems with systems not using wave reflection
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S15/00—Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
    • G01S15/88—Sonar systems specially adapted for specific applications
    • G01S15/93—Sonar systems specially adapted for specific applications for anti-collision purposes
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft

Abstract

The invention discloses a water source detection device for underground water source detection, which belongs to the technical field of water source detection and comprises a detection device and a machine body, wherein the detection device is arranged inside the machine body, the machine body comprises a machine room, flight wings, a flight control device and a remote controller, a steel frame is wrapped outside the machine room, four fixed wing connecting rods are fixedly connected outside the steel frame, a battery I is arranged at the bottom of the inner side of the machine room and supplies power to all electric elements, a partition plate is arranged above the battery I, the outer side of the partition plate is fixedly connected with the inner wall of the machine room, four power motors are fixedly connected above the partition plate, a gear I is arranged on an output shaft of each power motor, the traditional water source detection device is mainly used for detecting water sources by a land bracket, the detection efficiency is low, time and labor are wasted, the device remotely controls and detects water sources by an unmanned flight device, the quick transposition can be carried out, one operation alright cover a slice region, labour saving and time saving.

Description

Water source detection device for underground water source detection
Technical Field
The invention relates to the technical field of water source detection, in particular to a water source detection device for underground water source detection.
Background
Groundwater resources are more complex than surface water resources, so the change of the quality and quantity of groundwater itself and the environmental conditions and migration rules of groundwater causing groundwater change cannot be directly observed, and meanwhile, groundwater pollution and ground settlement caused by groundwater super-mining are slow-varying types, and once the underground water pollution and the ground settlement are accumulated to a certain degree, irreversible damage is caused. Therefore, the groundwater must be monitored for a long time to accurately develop and protect the groundwater, and the dynamic change condition must be mastered in time.
The satellite gravity method is adopted to detect the high cost, the manual detection area is limited, and the nuclear magnetic resonance method is adopted to detect the high cost of water source equipment, so that a simple and rapid multi-point detection device is needed to measure the overall condition of the underground water source.
Disclosure of Invention
In order to solve the technical problem, the invention provides a water source detection device for underground water source detection.
The technical scheme of the invention is as follows: a water source detection device for underground water source detection comprises a detection device and a machine body, wherein the detection device is installed inside the machine body, the machine body comprises a machine room, a flight wing, a flight control device and a remote controller, a steel frame is wrapped outside the machine room, four fixed wing connecting rods are fixedly connected to the outside of the steel frame, a first battery is arranged at the bottom of the inner side of the machine room and supplies power to the first battery, a partition plate is arranged above the first battery, the outer side of the partition plate is fixedly connected with the inner wall of the machine room, four power motors are fixedly connected to the upper side of the partition plate, a first gear is arranged on an output shaft of each power motor, a rotating shaft is rotatably connected in the fixed wing connecting rods, a second gear is arranged at the inner end of the rotating shaft, a third gear is arranged at the outer end of the rotating shaft, the second gear is in meshing transmission with the first gear, and four flight wings are arranged, the lower ends of the four flight wings are respectively in meshing transmission with the gear III, the flight control device is fixedly connected above the partition plate, and the remote controller is wirelessly connected with the flight control device;
the detection device comprises two water source detection probes and two water source detectors, wherein the two water source detection probes are respectively arranged on two sides below the engine room, and the water source detectors are fixedly connected above the partition plate and electrically connected with the water source detection probes and the flight control device.
Further, remote controller includes remote controller shell, flight remote controller, display, control button, battery two, flight remote controller fixed connection is in the inside right side of remote controller shell, the embedded fixed connection of display is in the upper surface of remote controller shell, control button establishes the both sides at the display, flight remote controller and display, control button electric connection, battery two is fixed in the inboard bottom of remote controller shell, and battery two is located the below of water source detector and flight remote controller, and battery two is the power supply of flight remote controller and display, receives flight data and water source detection data through flight controller, and rethread flight controller sends flight parameter and control detection device and detects.
Further, the inboard of flying control device is equipped with the support, the inboard of support is equipped with the gyroscope that is used for the perception flight gesture, the outside of support is equipped with the protective housing, the gyroscope with fly control device electric connection, the gyroscope can the perception flight gesture, and can make the cabin remain stable.
Furthermore, the both sides of protective housing fixedly connected with respectively are used for detecting flying height's baroceptor and are used for the ultrasonic sensor of low latitude height accurate control, can effectively perceive flying height and low latitude obstacle.
Furthermore, two sides of the steel frame are respectively and fixedly connected with a U-shaped landing support for ground support, and the U-shaped landing supports are used for landing.
Further, the cabin bottom is equipped with the cloud platform, it is connected with the high definition appearance of making a video recording to rotate on the cloud platform, the high definition make a video recording the appearance with flight control device electric connection passes the landform topography back remote controller through the high definition appearance of making a video recording.
Further, the water source detection probe comprises a fixing frame, a steering engine and a power-on conductor, two fixing sleeves are fixedly connected to the outer side of the fixing frame, a rotating cylinder is rotatably connected between the two fixing sleeves, a gear four is arranged on the outer side of the rotating cylinder, the steering engine is fixedly connected to the inner side of the fixing frame, a gear five is arranged on an output shaft of the steering engine, the gear four is in meshing transmission with the gear five, the power-on conductor is located inside the rotating cylinder and is in transmission connection with a screw rod on the inner wall of the rotating cylinder, and the water source detection probe descends in a screw rod transmission mode.
Furthermore, the outer wall of the upper part of the electrified conductor is wrapped with an insulating sleeve, so that the electrified conductor is prevented from electric leakage.
Furthermore, cabin lateral wall fixedly connected with anticollision connecting rod, the outside of anticollision connecting rod is equipped with the anticollision ring, can effectively place the striking of barrier to the cabin, increases the security in cabin.
Furthermore, the flight wing includes screw, connecting cylinder, wing axle, the wing axle with the connecting cylinder rotates to be connected, the below inner wall of connecting cylinder with fixed wing connecting rod threaded connection, the lower extreme of wing axle is equipped with gear six, gear six with gear three meshing transmission carries out the transmission through the wing axle.
The invention has the beneficial effects that:
(1) traditional water source detection device mostly is land support and detects, and detection efficiency is low, wastes time and energy, and this device passes through unmanned aerial vehicle device, and remote control detects the water source, can replace fast, and an operation alright covers a slice region, labour saving and time saving.
(2) The device carries out water source detection through an electrical method, and the detection device is low in cost, suitable for detection of various terrains and low in environmental influence factor.
Drawings
Fig. 1 is a schematic structural view of the present invention.
Fig. 2 is an enlarged view at a in fig. 1.
Fig. 3 is a schematic structural diagram of the remote controller.
Fig. 4 is a schematic structural view of a water source detecting needle.
Wherein, 1-detection device, 2-machine body, 21-cabin, 22-flying wing, 23-flying control device, 24-remote controller, 211-steel frame, 212-fixed wing connecting rod, 213-battery I, 214-clapboard, 215-power motor, 216-gear I, 217-rotating shaft, 218-gear II, 219-gear III, 11-water source detection probe, 12-water source detector, 241-remote controller shell, 242-flying remote controller, 243-display, 244-control button, 245-battery II, 231-bracket, 232-gyroscope, 233-protective shell, 2331-air pressure sensor, 2332-ultrasonic sensor, 2111-landing bracket, 2114-cradle head, 2115-high-definition camera, 111-a fixed frame, 112-a steering engine, 113-a power-on conductor, 114-a fixed sleeve, 115-a rotating cylinder, 116-a gear four, 117-a gear five, 1131-an insulating sleeve, 2112-an anti-collision connecting rod, 2113-an anti-collision ring, 221-a propeller, 222-a connecting cylinder, 223-a wing shaft and 224-a gear six.
Detailed Description
Example 1:
as shown in fig. 1, a water source detecting device for detecting an underground water source comprises a detecting device 1 and a machine body 2, wherein the detecting device 1 is installed inside the machine body 2, the machine body 2 comprises a machine cabin 21, flying wings 22, a flying control device 23 and a remote controller 24, the outer side of the machine cabin 21 is wrapped by a steel frame 211, the outer side of the steel frame 211 is fixedly connected with four fixed wing connecting rods 212, the bottom of the inner side of the machine cabin 21 is provided with a battery I213, the battery I213 supplies power for each power consumption element, a partition plate 214 is arranged above the battery I213, the outer side of the partition plate 214 is fixedly connected with the inner wall of the machine cabin 21, four power motors 215 are fixedly connected above the partition plate 214, a gear I216 is arranged on an output shaft of each power motor 215, a rotating shaft 217 is rotatably connected in the fixed wing connecting rods 212, a gear II 218 is arranged at the inner end of the rotating shaft 217, a gear III 219 is arranged at the outer end of the rotating shaft 217, and the gear II 218 is in meshing transmission with the gear I216, the number of the flight wings 22 is four, the lower ends of the four flight wings 22 are respectively in meshed transmission with the gear III 219, the flight control device 23 is fixedly connected above the partition plate 214, and the remote controller 24 is wirelessly connected with the flight control device 23;
detection device 1 includes water source detection probe 11, water source detector 12, and water source detection probe 11 has two, and two water source detection probes 11 are installed respectively in cabin 21 below both sides, and water source detector 12 fixed connection is in baffle 214 top, and with water source detection probe 11 and flight control device 23 electric connection.
As shown in fig. 3, the remote controller 24 includes a remote controller case 241, a flight remote controller 242, a display 243, a control button 244, and a second battery 245, the flight remote controller 242 is fixedly connected to the right side inside the remote controller case 241, the display 243 is fixedly connected to the upper surface of the remote controller case 241 in an embedded manner, the control button 244 is disposed on two sides of the display 243, the flight remote controller 242 is electrically connected to the display 243 and the control button 244, the second battery 245 is fixed at the bottom inside the remote controller case 241, the second battery 245 is located below the water source detector 12 and the flight remote controller 242, the second battery 245 supplies power to the flight remote controller 242 and the display 243, receives flight data and water source detection data through the flight controller 242, and sends flight parameters and controls the detection device 1 to perform detection through the flight controller 242.
The support 231 is arranged on the inner side of the flight control device 23, the gyroscope 232 used for sensing the flight attitude is arranged on the inner side of the support 231, the protective shell 233 is arranged on the outer side of the support 231, the gyroscope 232 is electrically connected with the flight control device 23, the gyroscope 232 can sense the flight attitude, and the cabin 21 can be kept stable.
An air pressure sensor 2331 for detecting flying height and an ultrasonic sensor 2332 for accurately controlling low altitude height are fixedly connected to both sides of the protective shell 233, respectively, so that flying height and low altitude obstacles can be effectively sensed.
Two sides of the steel frame 211 are respectively fixedly connected with a U-shaped landing bracket 2111 for ground support, for landing.
Cabin 21 bottom is equipped with cloud platform 2114, and cloud platform 211 is last to rotate to be connected with high definition camera 2115, and high definition camera 2115 and flight control device 23 electric connection pass back remote controller 24 with the landform topography through high definition camera 2115.
As shown in fig. 4, the water source detecting probe 11 includes a fixing frame 111, a steering gear 112, and an electrified conductor 113, two fixing sleeves 114 are fixedly connected to an outer side of the fixing frame 111, a rotating cylinder 115 is rotatably connected between the two fixing sleeves 114, a gear four 116 is arranged on an outer side of the rotating cylinder 115, the steering gear 112 is fixedly connected to an inner side of the fixing frame 111, a gear five 117 is arranged on an output shaft of the steering gear 112, the gear four 116 is in meshing transmission with the gear five 117, the electrified conductor 113 is located inside the rotating cylinder 115 and is in transmission connection with a screw rod on an inner wall of the rotating cylinder 115, and the water source detecting probe 11 is lowered in a screw rod transmission manner.
As shown in fig. 2, the flying wing 22 includes a propeller 221, a connecting cylinder 222, and a wing shaft 223, the wing shaft 223 is rotatably connected to the connecting cylinder 222, the lower inner wall of the connecting cylinder 222 is in threaded connection with the fixed wing connecting rod 212, a gear six 224 is provided at the lower end of the wing shaft 223, and the gear six 224 is in mesh transmission with a gear three 219 and is in transmission through the wing shaft 223.
Example 2:
as shown in fig. 1, a water source detecting device for detecting an underground water source comprises a detecting device 1 and a machine body 2, wherein the detecting device 1 is installed inside the machine body 2, the machine body 2 comprises a machine cabin 21, flight wings 22, a flight control device 23 and a remote controller 24, the outer side of the machine cabin 21 is wrapped by a steel frame 211, four fixed wing connecting rods 212 are fixedly connected to the outer side of the steel frame 211, a battery I213 is arranged at the bottom of the inner side of the machine cabin 21, the battery I213 supplies power for each power consumption element, a partition plate 214 is arranged above the battery I213, the outer side of the partition plate 214 is fixedly connected with the inner wall of the machine cabin 21, four power motors 215 are fixedly connected above the partition plate 214, a gear I216 is arranged on an output shaft of each power motor 215, a rotating shaft 217 is rotatably connected to the fixed wing connecting rods 212, a gear II 218 is arranged at the inner end of the rotating shaft 217, a gear III 219 is arranged at the outer end of the rotating shaft 217, the gear II 218 is in meshing transmission with the gear I216, the lower ends of the four flying wings 22 are respectively in meshed transmission with a gear III 219, the flying control device 23 is fixedly connected above the partition plate 214, and the remote controller 24 is wirelessly connected with the flying control device 23;
detection device 1 includes water source detection probe 11, water source detector 12, and water source detection probe 11 has two, and two water source detection probes 11 are installed respectively in cabin 21 below both sides, and water source detector 12 fixed connection is in baffle 214 top, and with water source detection probe 11 and flight control device 23 electric connection.
As shown in fig. 3, the remote controller 24 includes a remote controller shell 241, a flight remote controller 242, a display 243, control buttons 244, and a second battery 245, the flight remote controller 242 is fixedly connected to the right side inside the remote controller shell 241, the display 243 is fixedly connected to the upper surface of the remote controller shell 241 in an embedded manner, the control buttons 244 are disposed on two sides of the display 243, the flight remote controller 242 is electrically connected to the display 243 and the control buttons 244, the second battery 245 is fixed at the bottom inside the remote controller shell 241, the second battery 245 is located below the water source detector 12 and the flight remote controller 242, the second battery 245 supplies power to the flight remote controller 242 and the display 243, receives flight data and water source detection data through the flight controller 242, and sends flight parameters and controls the detection device 1 for detection through the flight controller 242.
The support 231 is arranged on the inner side of the flight control device 23, the gyroscope 232 used for sensing the flight attitude is arranged on the inner side of the support 231, the protective shell 233 is arranged on the outer side of the support 231, the gyroscope 232 is electrically connected with the flight control device 23, the gyroscope 232 can sense the flight attitude, and the cabin 21 can be kept stable.
An air pressure sensor 2331 for detecting flying height and an ultrasonic sensor 2332 for accurately controlling low altitude height are fixedly connected to both sides of the protective shell 233, respectively, so that flying height and low altitude obstacles can be effectively sensed.
Two sides of the steel frame 211 are respectively and fixedly connected with a U-shaped landing bracket 2111 for ground support, and the U-shaped landing bracket is used for landing.
The bottom of the cabin 21 is provided with a cloud deck 2114, the cloud deck 211 is connected with a high-definition camera 2115 in a rotating mode, the high-definition camera 2115 is electrically connected with the flight control device 23, and the landform and the terrain are transmitted back to the remote controller 24 through the high-definition camera 2115.
As shown in fig. 4, the water source detection probe 11 includes a fixed frame 111, a steering gear 112, and an electrified conductor 113, two fixed sleeves 114 are fixedly connected to the outer side of the fixed frame 111, a rotating cylinder 115 is rotatably connected between the two fixed sleeves 114, a gear four 116 is arranged on the outer side of the rotating cylinder 115, the steering gear 112 is fixedly connected to the inner side of the fixed frame 111, a gear five 117 is arranged on an output shaft of the steering gear 112, the gear four 116 is in meshing transmission with the gear five 117, the electrified conductor 113 is located inside the rotating cylinder 115 and is in transmission connection with a screw rod on the inner wall of the rotating cylinder 115, and the water source detection probe 11 is lowered in a screw rod transmission manner.
The outer side wall of the cabin 21 is fixedly connected with an anti-collision connecting rod 2112, an anti-collision ring 2113 is arranged on the outer side of the anti-collision connecting rod 2112, so that the impact of obstacles on the cabin 21 can be effectively prevented, and the safety of the cabin 21 is improved.
As shown in fig. 2, the flying wing 22 includes a propeller 221, a connecting cylinder 222, and a wing shaft 223, the wing shaft 223 is rotatably connected to the connecting cylinder 222, the lower inner wall of the connecting cylinder 222 is in threaded connection with the fixed wing connecting rod 212, a gear six 224 is provided at the lower end of the wing shaft 223, and the gear six 224 is in mesh transmission with a gear three 219 and is in transmission through the wing shaft 223.
Example 2 compared to example 1, example 2 adds a bump ring 2113 to reduce damage to the flight wing 22 of an aircraft, even if the aircraft crashes.
Example 3:
as shown in fig. 1, a water source detecting device for detecting an underground water source comprises a detecting device 1 and a machine body 2, wherein the detecting device 1 is installed inside the machine body 2, the machine body 2 comprises a machine cabin 21, flying wings 22, a flying control device 23 and a remote controller 24, the outer side of the machine cabin 21 is wrapped by a steel frame 211, the outer side of the steel frame 211 is fixedly connected with four fixed wing connecting rods 212, the bottom of the inner side of the machine cabin 21 is provided with a battery I213, the battery I213 supplies power for each power consumption element, a partition plate 214 is arranged above the battery I213, the outer side of the partition plate 214 is fixedly connected with the inner wall of the machine cabin 21, four power motors 215 are fixedly connected above the partition plate 214, a gear I216 is arranged on an output shaft of each power motor 215, a rotating shaft 217 is rotatably connected in the fixed wing connecting rods 212, a gear II 218 is arranged at the inner end of the rotating shaft 217, a gear III 219 is arranged at the outer end of the rotating shaft 217, and the gear II 218 is in meshing transmission with the gear I216, the lower ends of the four flying wings 22 are respectively in meshed transmission with a gear III 219, the flying control device 23 is fixedly connected above the partition plate 214, and the remote controller 24 is wirelessly connected with the flying control device 23;
detection device 1 includes water source detection probe 11, water source detector 12, and water source detection probe 11 has two, and two water source detection probes 11 are installed respectively in cabin 21 below both sides, and water source detector 12 fixed connection is in baffle 214 top, and with water source detection probe 11 and flight control device 23 electric connection.
As shown in fig. 3, the remote controller 24 includes a remote controller case 241, a flight remote controller 242, a display 243, a control button 244, and a second battery 245, the flight remote controller 242 is fixedly connected to the right side inside the remote controller case 241, the display 243 is fixedly connected to the upper surface of the remote controller case 241 in an embedded manner, the control button 244 is disposed on two sides of the display 243, the flight remote controller 242 is electrically connected to the display 243 and the control button 244, the second battery 245 is fixed at the bottom inside the remote controller case 241, the second battery 245 is located below the water source detector 12 and the flight remote controller 242, the second battery 245 supplies power to the flight remote controller 242 and the display 243, receives flight data and water source detection data through the flight controller 242, and sends flight parameters and controls the detection device 1 to perform detection through the flight controller 242.
The support 231 is arranged on the inner side of the flight control device 23, the gyroscope 232 used for sensing the flight attitude is arranged on the inner side of the support 231, the protective shell 233 is arranged on the outer side of the support 231, the gyroscope 232 is electrically connected with the flight control device 23, the gyroscope 232 can sense the flight attitude, and the cabin 21 can be kept stable.
An air pressure sensor 2331 for detecting flying height and an ultrasonic sensor 2332 for accurately controlling low altitude height are fixedly connected to both sides of the protective shell 233, respectively, so that flying height and low altitude obstacles can be effectively sensed.
Two sides of the steel frame 211 are respectively and fixedly connected with a U-shaped landing bracket 2111 for ground support, and the U-shaped landing bracket is used for landing.
Cabin 21 bottom is equipped with cloud platform 2114, and cloud platform 211 is last to rotate to be connected with high definition camera 2115, and high definition camera 2115 and flight control device 23 electric connection pass back remote controller 24 with the landform topography through high definition camera 2115.
As shown in fig. 4, the water source detection probe 11 includes a fixed frame 111, a steering gear 112, and an electrified conductor 113, two fixed sleeves 114 are fixedly connected to the outer side of the fixed frame 111, a rotating cylinder 115 is rotatably connected between the two fixed sleeves 114, a gear four 116 is arranged on the outer side of the rotating cylinder 115, the steering gear 112 is fixedly connected to the inner side of the fixed frame 111, a gear five 117 is arranged on an output shaft of the steering gear 112, the gear four 116 is in meshing transmission with the gear five 117, the electrified conductor 113 is located inside the rotating cylinder 115 and is in transmission connection with a screw rod on the inner wall of the rotating cylinder 115, and the water source detection probe 11 is lowered in a screw rod transmission manner.
The outer wall of the upper portion of the current conductor 113 is wrapped with an insulating sleeve 1131 to prevent the current conductor from leaking.
The outer side wall of the cabin 21 is fixedly connected with an anti-collision connecting rod 2112, an anti-collision ring 2113 is arranged on the outer side of the anti-collision connecting rod 2112, the collision of obstacles to the cabin 21 can be effectively prevented, and the safety of the cabin 21 is improved.
As shown in fig. 2, the flying wing 22 includes a propeller 221, a connecting cylinder 222, and a wing shaft 223, the wing shaft 223 is rotatably connected to the connecting cylinder 222, the lower inner wall of the connecting cylinder 222 is in threaded connection with the fixed wing connecting rod 212, a gear six 224 is provided at the lower end of the wing shaft 223, and the gear six 224 is in mesh transmission with a gear three 219 and is in transmission through the wing shaft 223.
Example 3 compared with example 2, in example 3, the insulating sleeve 1131 is added to the outside of the current conductor, and the current leakage of the current conductor 113 can be effectively prevented.
The working method of the water source detection device for detecting the underground water source comprises the following steps:
s1: the airplane is started through the remote controller 24, the flight control device 23 controls the power motor 215 to rotate, so as to drive the rotating shaft 217 to rotate, and the rotating shaft 217 rotates to drive the four flying wings 22 to rotate, so as to realize flying;
s2: the landform and the landform are observed in high air through the high-definition camera 2115, the altitude is sensed through the air pressure sensor 2331, the flying attitude of the airplane is sensed through the gyroscope 232,
s3: after the airplane arrives at a designated place, a proper landing position is observed through the high-definition camera 2115, ground obstacles are sensed through the ultrasonic sensor 2332, and the rotating speed of the power motor 215 is slowly reduced, so that the landing support 2111 is stable;
s4: the steering engine rotates to drive the gear five to rotate, the gear five and the gear four are in meshing transmission to drive the rotating cylinder to rotate, the rotating cylinder 115 and the insulating sleeve 1131 on the outer side of the electrified conductor 113 are in screw transmission, and then the electrified conductor 113 is in contact with the ground to detect a water source
The flight control device 23, the remote controller 24, the power motor 215, the water source detector 12, the gyroscope 232, the air pressure sensor 2331, the ultrasonic sensor 2332, the high-definition camera 2115 and the steering engine 112 used in the above embodiments are all commercially available products as long as the functions of the present invention can be realized, and those skilled in the art can select and use the flight control device according to the general knowledge, and are not limited herein.

Claims (10)

1. The water source detection device for underground water source detection is characterized by comprising a detection device (1) and a machine body (2), wherein the detection device (1) is installed inside the machine body (2), the machine body (2) comprises a cabin (21), flight wings (22), a flight control device (23) and a remote controller (24), the outer side of the cabin (21) is wrapped by a steel frame (211), four fixed wing connecting rods (212) are fixedly connected to the outer side of the steel frame (211), a first battery (213) is arranged at the bottom of the inner side of the cabin (21), the first battery (213) supplies power for all power consumption elements, a partition plate (214) is arranged above the first battery (213), the outer side of the partition plate (214) is fixedly connected with the inner wall of the cabin (21), four power motors (215) are fixedly connected to the upper side of the partition plate (214), and a first gear (216) is arranged on an output shaft of each power motor (215), a rotating shaft (217) is rotationally connected to the fixed wing connecting rod (212), a second gear (218) is arranged at the inner end of the rotating shaft (217), a third gear (219) is arranged at the outer end of the rotating shaft (217), the second gear (218) is in meshing transmission with the first gear (216), four flight wings (22) are provided, the lower ends of the four flight wings (22) are in meshing transmission with the third gear (219) respectively, the flight control device (23) is fixedly connected above the partition plate (214), and the remote controller (24) is in wireless connection with the flight control device (23);
detection device (1) includes water source test probe (11), water source detector (12), water source test probe (11) have two, and two water source test probe (11) are installed respectively cabin (21) below both sides, water source detector (12) fixed connection be in baffle (214) top, and with water source test probe (11) and flight control device (23) electric connection.
2. The water source detecting apparatus for groundwater source detection as claimed in claim 1, the remote controller (24) comprises a remote controller shell (241), a flight remote controller (242), a display (243), a control button (244) and a battery II (245), the flying remote controller (242) is fixedly connected to the right side inside the remote controller shell (241), the display (243) is fixedly connected to the upper surface of the remote controller shell (241) in an embedded mode, the control buttons (244) are arranged on two sides of the display (243), the flight remote controller (242) is electrically connected with the display (243) and the control buttons (244), the second battery (245) is fixed at the bottom of the inner side of the remote controller shell (241), the second battery (245) is positioned below the water source detector (12) and the flight remote controller (242), and the second battery (245) supplies power for the flight remote controller (242) and the display (243).
3. The water source detection device for detecting the underground water source as claimed in claim 1, wherein a bracket (231) is arranged at the inner side of the flight control device (23), a gyroscope (232) for sensing the flight attitude is arranged at the inner side of the bracket (231), a protective shell (233) is arranged at the outer side of the bracket (231), and the gyroscope (232) is electrically connected with the flight control device (23).
4. The water source detecting apparatus for groundwater source detection as claimed in claim 3, wherein an air pressure sensor (2331) for detecting a flying height and an ultrasonic sensor (2332) for precisely controlling a low altitude height are fixedly connected to both sides of the protecting case (233), respectively.
5. The water source detecting apparatus for groundwater source detection according to claim 1, wherein a U-shaped lowering bracket (2111) for ground support is fixedly connected to each side of the steel frame (211).
6. The water source detection device for detecting the underground water source as claimed in claim 1, wherein a cloud deck (2114) is arranged at the bottom of the cabin (21), a high-definition camera (2115) is rotatably connected to the cloud deck (211), and the high-definition camera (2115) is electrically connected to the flight control device (23).
7. The water source detection device for detecting the underground water source as claimed in claim 1, wherein the water source detection probe (11) comprises a fixed frame (111), a steering engine (112) and an electrified conductor (113), two fixed sleeves (114) are fixedly connected to the outer side of the fixed frame (111), a rotating cylinder (115) is rotatably connected between the two fixed sleeves (114), a gear four (116) is arranged on the outer side of the rotating cylinder (115), the steering engine (112) is fixedly connected to the inner side of the fixed frame (111), a gear five (117) is arranged on an output shaft of the steering engine (112), the gear four (116) is in meshing transmission with the gear five (117), and the electrified conductor (113) is located inside the rotating cylinder (115) and is in transmission connection with a screw rod on the inner wall of the rotating cylinder (115).
8. A water source detection device for groundwater source detection as claimed in claim 7, wherein the upper outer wall of the current-carrying conductor (113) is wrapped with an insulating sleeve (1131).
9. The water source detecting device for detecting the underground water source according to claim 1, wherein an anti-collision connecting rod (2112) is fixedly connected to the outer side wall of the cabin (21), and an anti-collision ring (2113) is arranged on the outer side of the anti-collision connecting rod (2112).
10. A water source detecting device for groundwater source detection according to claim 1, wherein a crash bar (2112) is fixedly connected to an outer side wall of the nacelle (21).
CN202210756781.1A 2022-06-29 2022-06-29 Water source detection device for underground water source detection Pending CN115079297A (en)

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